View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 24253.46897639 .00000820 00000-0 28134-3 0 9996
2 27386 98.2908 211.6642 0001221 88.0230 21.7640 14.38665619180696
| Epoch (UTC): | 09 September 2024 11:15:19 |
| Eccentricity: | 0.0001221 |
| inclination: | 98.2908° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 211.6642° |
| argument of perigee: | 88.0230° |
| revolutions per day: | 14.38665619 |
| mean anomaly at epoch: | 21.7640° |
| orbit number at epoch: | 18069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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